Rapidly making a contoured part

Abstract: Method of rapidly producing a contoured part, comprising: designing a computer graphic model of the part, sectioning the graphic model into graphic members which are at least one of blocks or slabs, carving a solid member (14-150mm in thickness) for each of the graphic members, the solid member being proportion to and enveloping such graphic members, the carving being carried out by accessing two or more sides (opposite sides) of such solid member to at least essentially duplicate the corresponding graphic member, and securing the carved solid members together to replicate the graphic model as a usable unitary part. The method can be modified to make castings by carving wax or foam solid members which are assembled to form an investment pattern, the was pattern being used in a shell mould casting steps and the foam pattern being used in evaporative casting steps.

Description: This invention relates generally to manufacturing and shaping of parts constituted of reasonably rigid material, and more particularly to rapid prototyping of such parts by sectioned object machining which facilitates free-form fabrication. It is becoming paramount that prototype parts and their associated tools be fabricated faster in free-form, at lower cost, particularly in metal shapes, have superior surface finish and require little or no remachining. Technology attempting to meet these objectives fall into generally four categories: extruding, spraying, curing and laminate forming. Each has significant disadvantages that fail to meet all of the objectives. Extrusion uses a heated nozzle to extrude hot wax or other polymer filaments, such as nylon, into a shape. It cannot be used to make metal parts; it is fragile, subject to delamination, and is expensive. Spraying can be either (i) an emulsion type where a binder is sprayed onto a metal powder which is subsequently laser sintered, or (ii) thermally sprayed at high temperature using a metal powder to produce a shape. Spraying is expensive, slow and produces a mediocre surface finish which is porous. Curing, often times referred to as stereo lithography, involves subjecting photo-sensitive polymer resins in thin layers to a laser beam for curing and thence repeating these steps to build up a part. It is generally slow, useful only for nonmetals and tooling, and requires expensive emission control measures because of the odorous materials. It also demands post machining because the surface is not stable during storage, is somewhat brittle, and is size limited. Prior art laminate forming involves cutting of metal plys, paper, plastic sheets or foam, by use of a laser beam, hot wire or mechanical cutter to make sheet-like cutouts; the cutouts are subsequently assembled to form a unit, Laminate forming first was carried out without a computer graphic guide, the cutter following a mechanical guide. More recently, the prior art has programmed the cutter to follow a computer model or graphic such as shown in U.S. Patent 4,675,825. The latter type of laminate forming has been used to shape metal, hut fails to eliminate post-machining of the unit, lacks high structural integrity because of the need to use very thin laminates, is incapable of making complex parts such as intricate engine cylinder heads, manifolds or engine blocks, and is slow due to the high number of handling and finishing operations resulting from the number of laminates The requirement of post-machining for state of the art laminate forming is a significant drawback. Machining used for this process works only to cut edges of the thin sheet metal (up to 12 mm) inhibiting full contour machining. When the sheets are assembled, the total surface will be somewhat ragged or stepped, requiring post-machining to obtain acceptable surface finishing. If the laminates are foam, paper or plastic, the same problem remains because of the inability to fully free-form the edges of the material; moreover, foam materials can produce a high degree of porosity in the final surface when assembled. DE-4124961 A1 describes a method of making a prototype body from drawings which are presented as CAD data. In the described method the model body is divided using software into individual body portions (3-6). A sub-body (30,41,51) corresponding to the respective model body portions (3-6) is cut out of a predetermined material and the individual sub-bodies are joined together to form the prototype. The individual sub-bodies (30,41,51) have a thickness ≤ 0.1 mm. The initial section thickness of each sub-body is greater than its eventual thickness and each sub-body requires to he milled to achieve the required thickness. There is no suggestion, however, that a sub-body can be subjected to a three-dimensional machining operation and, indeed, the fragile, ≤ 0.1 mm thick, sub-bodies would not allow this. It is an object of this invention to rapidly make a contoured part by a more economical sectioned-object machining technique adaptable to the most complex parts, the method resulting in an immediate assembled surface finish that is superior, and the method having little or no disadvantageous manufacturing side effects. According to the present invention we provide a method of making a contoured functional part, comprising steps; (a) designing a computer graphic model of said part; (b) sectioning said graphic model into a plurality of graphic members; (c) developing a computer program for a cutting machine to cut a plurality of individual solid members corresponding to the contours of said plurality of graphic members; (d) providing individual solid members, each having a thickness that envelopes one of the corresponding stratiforms; and (e) securing an assembly of said solid members into an integral unit to constitute said part; characterised in that (i) each graphic member, and in turn each solid member, has a thickness that exceeds 14 millimetres; (ii) the said computer program is developed for a three-axis cutting machine; and (iii) between steps (d) and (e) each solid member is secured in a precise location and cut with said three-axis cutting machine by use of a cutting axis to at least two sides of said member to produce machined solid members. In step (c) a solid member is cut for each graphic member that is proportional to and envelopes such graphic member, such cutting being carried out by accessing two or more sides of such solid member to at least essentially duplicate the corresponding graphic member. Cutting is carried out on opposite sides of each member, such as by CNC milling machines, the thickness of the solid members being in the range of 14-150 mm and each of the solid members having opposed sides which are parallel or skewed with respect to each other. The method is capable of being applied to the making of unique machined metal functional parts, to the making of rapid developmental prototypes of cast metal parts, and to the rapid making of initial or preproduction cast components. The invention will now be described further, by way of example, with reference to the accompanying drawings, in which; Figure 1 is a block diagram of a process embodying the principles of this invention; Figure 2 is a perspective view of a computer graphic model of an engine head design having a single cylinder; Figure 2A is a view like 2, but showing additional design work such as bosses, locating holes, or bolt holes; Figure 3A is a schematic plan for taking sections or slices of the graphic model; Figure 3B is an elevational view of Figure 3A; Figure 4A is schematic elevational view of a plan for taking a combination of both vertical and horizontal slices or sections of the computer model; Figure 4B is a side view of the plan shown in Figure 4A; Figure 5 is an exploded perspective view of selected computer sections of the model of Figure 2, the sections being selected to facilitate opposite side machining; Figure 6 is an exploded perspective view of computer sections that create slabs of the design shown in Figures 2A and 2B; Figure 7 is a perspective view of the computerised cutting path which has been determined to carry out cutting of the top side of the fourth graphic member (37) in Figure 6 and thereby the fourth solid member; Figure 8 is a perspective view like that in Figure 7, but for a cutting path for the bottom of the fourth graphic member (37) and thereby the fourth solid member; Figure 9 is a perspective schematic view of a typical three-axis milling machine cutter as applied to the cutting of the top side of a solid member; Figure 10 is an exploded view of the solid members after machining, and as assembled together with brazing sheets there between; Figure 11 is a schematic flow diagram depicting how the method of this invention can be applied to the fast prototyping of cast components; and Figure 12 is a schematic flow diagram of how the method of this invention can be applied to the rapid making of initial preproduction cast components. The method of this invention machines a plurality of stratiform members which together, when assembled, constitute a desired part. The stratiform members are relatively thick sections of the part, herein called slabs or blocks, which demand as well as facilitate two-side machining (preferably opposite sides) controlled by computerised three axis milling machines. The fabrication time for the part will be significantly reduced and the method will be particularly effective when making a complex, multi-cored cast part such as an engine cylinder head or engine block. As shown in Figure 1, the method comprises four basic steps, the first three of which are carried out within or under the control of a programmed computer. The design of the computer graphic/model should be a three dimensional CAD (computer aided design) solid model or fully surfaced model such as the single cylinder engine head shown in Figure 2. Constraints must be given to the computer to control the design in certain parameters, such as solid stock size to be machined, direction of machine tool access, and the finish desired on the completed part. The design may also involve the placement of assembly or securing bolt openings which do not interrupt the internal functional cavities as shown in Figure 2A. In this graphic, the head 10 has a central combustion chamber roof 11, intake passages 14,15, and exhaust passages 12,13, along with a plurality of valve seats 16 for each of the passages. Several bosses are defined including spark plug or fuel injector boss 17, valve guide bosses 18 and joining bosses 19. It is important to plan the sectioning of the graphic model according to the block or slab concept of this invention, taking into account the location, size and shape of the internal cavities of the part to be produced. For example, as shown in Figures 3A and 3B, if the internal cavities 24,25 are located in vertically spaced rows and if the cavities 24,25 widely overlap in plan view, horizontal sectioning through each row of cavities is desirable to expose all of the cavities to proper access by the milling cutter. Such sectioning may be constrained by the minimal thickness that can be used to achieve a stable block or slab according to this invention. Such stable minimum thickness is about 14mm for metals such as aluminium and steel. Such minimum thickness may be adjusted based upon the strength of an alternative material. Such minimum thickness and strength is necessitated by the need for full three axis contour machining, not merely vertical cutting as with sheet metal. It may be practicable, in certain cases, to combine both horizontal and vertical sectioning planes, such as shown in Figures 4A and 4B, where the lower series of cavities 26 are enveloped within the plan view of the upper cavities 27. Still another alternative is to utilise only vertical sectioning such as shown in Figure 5. Such sectioning may also create steps in the slabs or blocks. The ability to expose properly the internal passages 28, 29, 30 and 31 is a criteria by which this sectioning should be selected. Here, such passages are generally in vertical planes 32 and 33. As shown in Figure 6, five sections or slices of different but uniform thicknesses were determined to optimally expose the interior cavities of the single cylinder engine head model of Figure 2. The slabs are graphic members 34, 35, 36, 37 and 38. Note the narrow thickness of slab 37, the greater thickness of slabs 35 and 36, and the still greater thickness of slabs 34 and 38. All of the slabs are of generally uniform thickness as a result of parallel horizontal sectioning. The complex contours and unusual shape of the exhaust passages 12,13 and intake passages 14,15 are exposed for three axis machining by the slabs 35-38, leaving no uncuttable areas or overhangs. The lack of complex contours in the top and bottom slabs 34,38 allow such slabs to have greater thickness. The sectioning of the computer graphic model is adapted to provide for overlap between the slabs or graphic members. Such overlapping aspect is necessary to maintain continuity between surfaces. In certain slabs or graphic members, the bosses defining certain cavities may be suspended and detached from the side walls 41 within that particular slab, thus necessitating the use of bridges 39,40 such as shown for slabs 36 and 37; such bridges may be later removed if necessary or desired. The surface quality of the machined solid members (slabs or blocks) is dependent on the surface requirements, preferably about .005mm when utilising material such as aluminium or steel. However, the surface finish can be adapted to the material being cut so that it is better than that normally provided by present industrial standards. The solid members (blocks or slabs) to be machined should have a size which is generally equal to or greater than the corresponding graphic member to thereby envelope all sides of the computer graphic member. Once the solid model has been sectioned into blocks or slabs, tool cutting paths must be derived by the computer program for the plurality of the exposed surfaces that are to be machined in each solid member (block or slab), preferably at the opposed top and bottom surfaces of horizontal sectioned solid members. Tool paths 44,45 for the single cylinder engine head are shown in Figures 7 and 8 for member 37. Tool path 44 is for top access to the member shown in Figure 7, and tool path 45 is for bottom access (the member turned over) to the member shown in Figure 8. The software that is utilised to derive such tool paths is generally known as Computer Visions®-CAD/CAM system, and consists of solid modelling, numerical control, and drafting. The tool paths, once generated, within the computer, are verified by Vericut® software. In carrying out the third step of the basic process, CNC milling is utilised to carve the various internal cavities and surfaces of each solid member (slab or block) while the solid member is rigidly fixed to the milling machine. It is desirable to drill locating openings for locator pins or alignment pins to facilitate holding or fixturing the solid member during subsequent machining, as shown in Figure 9. The locator openings and joining openings will also determine the exact reassembly of the solid members (slabs and blocks) as a unit. The bolt holes (that may be utilised to secure the assembly in some cases) should be drilled with precise accuracy. It is important that the milling machine be able to remove material in the X, Y and Z axes to create a duplicate of the graphic model. An example of a CNC milling machine that may be utilised for purposes of carrying out this step of the process is shown in Figure 9. Although only three axis milling is needed, the method can utilise four or five axis milling also, but it may not be necessary. In the final step of the basic process, the individual slabs or blocks should be preferably cleaned to remove all oxides in the event that securing is by brazing, soldering, or adhesive requiring some form of substance action. In the example of the single cylinder engine head, the slabs are assembled together after cleaning with brazing foil or sheets 47 superimposed between members 34-38 as shown in Figure 10; locating pins 48 are introduced to aligning openings 51 to precisely bring the solid members (slabs) together in the exact location needed to duplicate the graphic model. Additionally, bolts or fasteners 50 may be employed through openings 52 to clamp the assembly together during handling within a furnace used for heat treatment to follow. The brazing material utilised for aluminium alloys is a eutectic aluminium Si-Mg braze foil, having the following chemistry: 83-90% Al, 9-13% Si, 0.1-1.75% Mg, 0-.15% Bi. The sheets of brazing material have a thickness in the range of .003-.010 inches. If other materials such as cast iron, alloy steels, or Mg alloys are used, a different suitable eutectic brazing or soldering material is used. After cleaning the assembly, the clamped unit is placed in a furnace in a suitable inert atmosphere with or without flux, and subjected to a precise heating cycle to complete brazing and effect a metallurgical bond between the brazing material and the slabs themselves. The unit is heated to a temperature that is roughly 30°C below the melting temperature of the solid members (slab metal) (about 595°C for aluminium). A subsequent cooling/heating cycle within the furnace may be used such as a T5 or T6 cycle. The method of this invention reduces the overall time period for producing a metal part by as much as 30%, reduces cost by typically 50%, and eliminates side effects such as distortion, instability of the assembled unit, brittleness, odorous emissions, limitations as to member material selection, and the need for rotating the solid member while machining. With respect to time reductions, it is now conventional to make metal prototypes by sequence which involves machining patterns, making a mould, and then casting parts. This will typically take 15 weeks. In contrast, the single cylinder head disclosed in the above description can be designed and produced within 3-4 weeks. The process eliminates waste, reduces the number of steps and personnel needed to perform, and permits use of a variety of materials such as cast iron, magnesium, steel, aluminium, and alloys thereof; all lead to cost reduction. The resulting product of this method comprises: a stack of solid members (blocks or slabs) secured together in sequence to replicate the three-dimensional computer graphic model of the part, the solid members (blocks or slabs) being prepared by the steps of (i) sectioning a graphic model into graphic members which are blocks and/or slabs, and (ii) carving a solid member (block or slab) for each of the graphic model members by accessing two or more sides of the solid members to essentially duplicate the corresponding graphic section members. Such product will possess valuable unique characteristics which comprise structural stability, an outer contoured smooth surface that is not interrupted or stepped from solid member to solid member (block to block or slab to slab), the surface finish and strength of the product being at least as good as that conventionally produced. For the solid members utilised in the basic method, metal is selected as normally required by the functional part. The sectioning must accommodate the condition of the solid member when reduced to stratiforms, while providing access to the designed internal cavities. The product eliminates stack-up errors characteristic of object sectioning using very thin laminations. As shown in Figure 11, the process can be first modified to rapidly produce cast (metal or synthetic) parts in prototype quantities at greatly reduced cost and time. Thus, the basic method would be used to create a nonfunctional part or tooling which then in turn is used to produce a cast part. The alternative method requires modifying step 3 by using wax (instead of metal) for the solid members to be carved. The solid members are carved, assembled into a unit to define an investment pattern. The pattern is coated with a ceramic shell to create a mould. The wax investment pattern is dipped and coated with ceramic slurry to form a surrounding shell which can function as a mould. The mould is preferably formed by dipping the pattern into a slurry consisting of a ceramic flour in colloidal silica and then sprinkling it with a fine sand. After drying, the mould is dipped into another ceramic slurry, then into a fluidised bed containing granular molochite thus stuccoing the surface again. The wax is removed by heat leaving the desired casting cavity, which is then filled with molten metal to form the prototype cast object precisely duplicating the computer graphic model. The investment wax pattern may be removed either by shock-firing or steam autoclaving. When metal is poured into the mould cavity to produce the required cast object, a precise and accurate casting is produced. Such method of producing castings provides superior and accurate surface quality when compared to other rapid prototyping techniques. The tool paths developed are closer to the production tool level and the sectioning of the computer model for a wax pattern can follow true parting lines needed for casting purposes. The process allows reduced fabrication time, thus giving greater lead time in designing new parts for automobiles and thereby earlier evaluation of competing designs. As a still further modification of the basic process, rapid production castings can be economically produced, for example, in quantities of 100 or less. As shown in Figure 12, such method involves carving of foam patterns, (comprised of polystyrene) by CNC milling machines which are guided by the computer graphic model. Such computer model foam pattern is again sectioned into members (blocks and slabs) for carrying out the machining of the internal cavities of the part. The foam solid members, after carving (machining) are assembled together in a unit and secured such as by microwave adhesion or by introducing a fluid adhesive to the mating surfaces of the solid members. The assembled foam pattern is then given a refractory coating and dried. The unitised foam members are inserted into an open chamber into which fluidised dry sand is introduced to surround and fill the foam pattern; the pattern assembly must also contain suitable foam gating members such as from stock foam parts. Molten metal is poured into the gating members of the foam pattern to displace and vaporise the foam, allowing gaseous emissions to migrate into the unbonded dry but compacted sand mould. The resulting casting will contain a precise definition of the computer designed production casting. This method modification is particularly valuable to produce limited preproduction castings.

Claims: A method of making a contoured functional part, comprising steps; (a) designing a computer graphic model (10) of said part; (b) sectioning said graphic model (10) into a plurality of graphic members; (c) developing a computer program for a cutting machine to cut a plurality of individual solid members corresponding to the contours of said plurality of graphic members; (d) providing individual solid members, each having a thickness that envelopes one of the corresponding stratiforms; and (e) securing an assembly of said solid members into an integral unit to constitute said part; characterised in that (i) each graphic member, and in turn each solid member, has a thickness that exceeds 14 millimetres; (ii) the said computer program is developed for a three-axis cutting machine; and (iii) between steps (d) and (e) each solid member is secured in a precise location and cut with said three-axis cutting machine by use of a cutting axis to at least two sides of said member to produce machined solid members (34,35,36,37,38). A method as claimed in claim 1, in which said graphic model is a solid model or a fully surfaced model. A method as claimed in either claim 1 or claim 2, in which the sectioning of step (b) is with parallel planes to create graphic slabs. A method as claimed in any one of claims 1 to 3, in which said solid members are metallic, the metal being selected from the group of aluminium, steel, cast iron, magnesium, and alloys thereof, and the thickness of each solid member is in the range of 14-150 millimetres. A method as claimed in any one of the preceding claims, in which securing in step (d) is by adhesive bonding or brazing. A method as claimed in claim 5, in which said securing in step (d) mates section surfaces of said solid members (34,35,36,37,38) to each other by brazing utilising high density magnesium as the brazing flux between section surfaces. A method as claimed in any one of the preceding claims, in which sectioning in step (b) uses one or more vertical and horizontal planes in combination. A method as claimed in either claim 5 or claim 6, in which the solid members are secured together by brazing wherein sheets of brazing foil (47) are inserted between the solid members (34,35,36,37,38) prior to assembly and then, after assembly, subjected to a heat treatment which comprises heating to a temperature of 595°C in a furnace and subsequently cooling the furnace. A rapidly produced contoured functional part produced by the method of any one of claims 1 to 8, the said integral unit produced in step (e) of claim 1 having an outer contoured smooth surface extending from solid member to solid member which is devoid of steps or raggedness and having a surface finish smooth to at least 0.01 mm.

Inventors: BROGLEY MARTIN ANDREW, BURCH CRAIG EDWARD, GRAB GERALD A, GRENKOWITZ ROBERT WALTER, NOVAK ROBERT FRANCIS, RIGLEY MICHAEL RAYMOND, SHAIKH FURGAN ZAFAR, SMITH GREGORY HUGH, BROGLEY, MARTIN ANDREW, BURCH, CRAIG EDWARD, GRAB, GERALD A., GRENKOWITZ, ROBERT WALTER, NOVAK, ROBERT FRANCIS, RIGLEY, MICHAEL RAYMOND, SHAIKH, FURGAN ZAFAR, SMITH, GREGORY HUGH
Applicants: FORD FRANCE, FORD MOTOR CO, FORD WERKE AG, FORD FRANCE S. A., FORD MOTOR COMPANY, FORD MOTOR COMPANY LIMITED, FORD-WERKE AKTIENGESELLSCHAFT
Application year: 1994
Main classification: G05B19
IPC codes: G05B19